Emax=WWmax-WWmin;/*--?求最大盈亏功 --*/РJF=900*EEmax/(PI*PI*140*140*dt);Рfputs(" 以下为运动分析结果?:\n",fp);Р1Рfputs("?φ φ 2?Sc?ω 2?Vc?α 2?ac\n",fp);Рfor(i=0;i<37;i++)Р{fprintf(fp,"%-3d?%-8.2f?%-8.3f %-8.3f?%-8.3f?%-8.3f?%-8.3f\n",10*i,Q2[i]*180/PI,sc[iР],w2[i],vc[i],aa2[i],ac[i]);Р}Рfputs("\n 以下为动力分析结果?:\n\n",fp);Рfputs("?φ 1?R43?R12?β 1?R23?β 2?R41?β 3?Mb0РMb\n",fp);Рfor(i=0;i<37;i++)Р{fprintf(fp,"%3d %7.2f %7.2f %7.2f %7.2f %7.2f %7.2f %7.2f %7.2f %7.2f\n",10*i,R43[i],R12[iР],b12[i],R23[i],b23[i],R41[i],b41[i],Mb0[i],Mb[i]);Р}Рfputs("\n 以下为飞轮设计结果?:\n\n",fp);Рfprintf(fp," 动力矩?Md=%.2f\n?平均功率为?%.2f\n 最大盈亏功为?%.2f\n 飞轮转动惯量РJF>=%.2f\n 飞轮矩= %.2f\n",Md,Md*w1,EEmax,JF,4*g*JF);Рfputs("?φ 1 Wr?Wd?ΔW\n",fp);Рfor(i=0;i<37;i++)Р{fprintf(fp,"%-3d?%-8.2f?%-7.2f?%-7.2f\n",10*i,(-1)*Wr[i],Wd[i],WW[i]);Р}Рfclose(fp);Р}